CN103032900B - 三元组反向旋转涡漩器和使用方法 - Google Patents

三元组反向旋转涡漩器和使用方法 Download PDF

Info

Publication number
CN103032900B
CN103032900B CN201310005639.4A CN201310005639A CN103032900B CN 103032900 B CN103032900 B CN 103032900B CN 201310005639 A CN201310005639 A CN 201310005639A CN 103032900 B CN103032900 B CN 103032900B
Authority
CN
China
Prior art keywords
fuel
circular cowling
vortex device
vortex
ring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201310005639.4A
Other languages
English (en)
Chinese (zh)
Other versions
CN103032900A (zh
Inventor
A.M.埃尔卡迪
A.T.埃武莱特
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN103032900A publication Critical patent/CN103032900A/zh
Application granted granted Critical
Publication of CN103032900B publication Critical patent/CN103032900B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
CN201310005639.4A 2006-11-17 2007-11-19 三元组反向旋转涡漩器和使用方法 Expired - Fee Related CN103032900B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/560,931 US8099960B2 (en) 2006-11-17 2006-11-17 Triple counter rotating swirler and method of use
US11/560931 2006-11-17
US11/560,931 2006-11-17

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CNA2007101870609A Division CN101182928A (zh) 2006-11-17 2007-11-19 三环形反向旋转涡漩器

Publications (2)

Publication Number Publication Date
CN103032900A CN103032900A (zh) 2013-04-10
CN103032900B true CN103032900B (zh) 2015-06-17

Family

ID=39092758

Family Applications (2)

Application Number Title Priority Date Filing Date
CNA2007101870609A Pending CN101182928A (zh) 2006-11-17 2007-11-19 三环形反向旋转涡漩器
CN201310005639.4A Expired - Fee Related CN103032900B (zh) 2006-11-17 2007-11-19 三元组反向旋转涡漩器和使用方法

Family Applications Before (1)

Application Number Title Priority Date Filing Date
CNA2007101870609A Pending CN101182928A (zh) 2006-11-17 2007-11-19 三环形反向旋转涡漩器

Country Status (5)

Country Link
US (1) US8099960B2 (de)
EP (1) EP1923637B1 (de)
JP (1) JP5331327B2 (de)
KR (1) KR101450874B1 (de)
CN (2) CN101182928A (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8479488B2 (en) * 2009-07-27 2013-07-09 General Electric Company Oxyfuel gas turbine system and method
US8381525B2 (en) * 2009-09-30 2013-02-26 General Electric Company System and method using low emissions gas turbine cycle with partial air separation
US8925323B2 (en) 2012-04-30 2015-01-06 General Electric Company Fuel/air premixing system for turbine engine
US9677766B2 (en) * 2012-11-28 2017-06-13 General Electric Company Fuel nozzle for use in a turbine engine and method of assembly
WO2014171991A2 (en) * 2013-02-01 2014-10-23 United Technologies Corporation Fuel injector for high altitude starting and operation of a gas turbine engine
US9377202B2 (en) 2013-03-15 2016-06-28 General Electric Company System and method for fuel blending and control in gas turbines
US9382850B2 (en) 2013-03-21 2016-07-05 General Electric Company System and method for controlled fuel blending in gas turbines
WO2015050601A2 (en) 2013-07-01 2015-04-09 United Technologies Corporation Enhanced apu operability
US9534788B2 (en) 2014-04-03 2017-01-03 General Electric Company Air fuel premixer for low emissions gas turbine combustor
US10480791B2 (en) 2014-07-31 2019-11-19 General Electric Company Fuel injector to facilitate reduced NOx emissions in a combustor system
KR20160027267A (ko) 2014-08-28 2016-03-10 한국기계연구원 와류 발생기를 장착한 예혼합 연소기 및 그 구동방법
WO2016122529A1 (en) * 2015-01-29 2016-08-04 Siemens Energy, Inc. Fuel injector including tandem vanes for injecting alternate fuels in a gas turbine
US20160265779A1 (en) * 2015-03-11 2016-09-15 General Electric Company Twin radial splitter-chevron mixer with converging throat
EP3115693B1 (de) * 2015-07-10 2021-09-01 Ansaldo Energia Switzerland AG Sequentielle brennkammer und verfahren zum betrieb davon
US10352567B2 (en) 2015-10-09 2019-07-16 General Electric Company Fuel-air premixer for a gas turbine
US10247106B2 (en) * 2016-06-15 2019-04-02 General Electric Company Method and system for rotating air seal with integral flexible heat shield
JP2018004138A (ja) * 2016-06-30 2018-01-11 川崎重工業株式会社 ガスタービン燃焼器
US11459959B2 (en) * 2016-09-16 2022-10-04 General Electric Company Method for starting a gas turbine
CN108031572B (zh) * 2017-12-13 2020-01-03 华中科技大学 一种自旋转中心体空化喷嘴
KR102691031B1 (ko) 2020-02-04 2024-08-01 한화에어로스페이스 주식회사 스월러 어셈블리 및 스월러 어셈블리의 제조방법
GB2611115B (en) * 2021-09-23 2024-10-09 Gen Electric Floating primary vane swirler
SE2250307A1 (en) * 2022-03-09 2023-09-10 Phoenix Biopower Ip Services Ab A method for the combustion of a fuel gas
US11835235B1 (en) 2023-02-02 2023-12-05 Pratt & Whitney Canada Corp. Combustor with helix air and fuel mixing passage
US11867400B1 (en) 2023-02-02 2024-01-09 Pratt & Whitney Canada Corp. Combustor with fuel plenum with mixing passages having baffles
US11873993B1 (en) 2023-02-02 2024-01-16 Pratt & Whitney Canada Corp. Combustor for gas turbine engine with central fuel injection ports
US12060997B1 (en) 2023-02-02 2024-08-13 Pratt & Whitney Canada Corp. Combustor with distributed air and fuel mixing
US11867392B1 (en) 2023-02-02 2024-01-09 Pratt & Whitney Canada Corp. Combustor with tangential fuel and air flow
US12111056B2 (en) 2023-02-02 2024-10-08 Pratt & Whitney Canada Corp. Combustor with central fuel injection and downstream air mixing

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5193346A (en) * 1986-11-25 1993-03-16 General Electric Company Premixed secondary fuel nozzle with integral swirler
US5165241A (en) * 1991-02-22 1992-11-24 General Electric Company Air fuel mixer for gas turbine combustor
US5251447A (en) * 1992-10-01 1993-10-12 General Electric Company Air fuel mixer for gas turbine combustor
US5351477A (en) * 1993-12-21 1994-10-04 General Electric Company Dual fuel mixer for gas turbine combustor
US5836164A (en) * 1995-01-30 1998-11-17 Hitachi, Ltd. Gas turbine combustor
US5680766A (en) * 1996-01-02 1997-10-28 General Electric Company Dual fuel mixer for gas turbine combustor
US5675971A (en) * 1996-01-02 1997-10-14 General Electric Company Dual fuel mixer for gas turbine combustor
US6141967A (en) * 1998-01-09 2000-11-07 General Electric Company Air fuel mixer for gas turbine combustor
US6272840B1 (en) * 2000-01-13 2001-08-14 Cfd Research Corporation Piloted airblast lean direct fuel injector
US6389815B1 (en) * 2000-09-08 2002-05-21 General Electric Company Fuel nozzle assembly for reduced exhaust emissions
US6453660B1 (en) * 2001-01-18 2002-09-24 General Electric Company Combustor mixer having plasma generating nozzle
US6986255B2 (en) * 2002-10-24 2006-01-17 Rolls-Royce Plc Piloted airblast lean direct fuel injector with modified air splitter
US6871501B2 (en) * 2002-12-03 2005-03-29 General Electric Company Method and apparatus to decrease gas turbine engine combustor emissions
US6862889B2 (en) * 2002-12-03 2005-03-08 General Electric Company Method and apparatus to decrease combustor emissions
JP4065947B2 (ja) * 2003-08-05 2008-03-26 独立行政法人 宇宙航空研究開発機構 ガスタービン燃焼器用燃料・空気プレミキサー
US6968693B2 (en) * 2003-09-22 2005-11-29 General Electric Company Method and apparatus for reducing gas turbine engine emissions
JP3944609B2 (ja) * 2003-12-16 2007-07-11 川崎重工業株式会社 燃料ノズル
EP1756252B1 (de) * 2004-04-28 2016-04-20 Sasol Technology (Pty) Ltd Verwendung von mischungen von dieselkraftstoff auf basis von rohöl und gas-to-liquids-dieselkraftstoff
GB2439097B (en) * 2006-06-15 2008-10-29 Rolls Royce Plc Fuel injector
US7631500B2 (en) * 2006-09-29 2009-12-15 General Electric Company Methods and apparatus to facilitate decreasing combustor acoustics
US20080163627A1 (en) * 2007-01-10 2008-07-10 Ahmed Mostafa Elkady Fuel-flexible triple-counter-rotating swirler and method of use

Also Published As

Publication number Publication date
KR101450874B1 (ko) 2014-10-14
US20080115501A1 (en) 2008-05-22
EP1923637A2 (de) 2008-05-21
CN103032900A (zh) 2013-04-10
JP2008128632A (ja) 2008-06-05
CN101182928A (zh) 2008-05-21
US8099960B2 (en) 2012-01-24
EP1923637A3 (de) 2013-12-11
JP5331327B2 (ja) 2013-10-30
KR20080045060A (ko) 2008-05-22
EP1923637B1 (de) 2018-08-01

Similar Documents

Publication Publication Date Title
CN103032900B (zh) 三元组反向旋转涡漩器和使用方法
RU2457397C2 (ru) Смеситель топлива с воздухом для камер сгорания
CN101158478B (zh) 用于运行涡轮发动机的方法和设备
US7581396B2 (en) Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers
EP1431543A2 (de) Turbinensystem und Injektor dafür
JP4997018B2 (ja) 一次燃料噴射器及び複数の二次燃料噴射ポートを有するガスタービンエンジン燃焼器のミキサ組立体のためのパイロットミキサ
US20140033722A1 (en) Fuel-Air Mixer For Use With A Combustor Assembly
CN101629719A (zh) 用于轴向分级的低排放燃烧器的附壁型喷射系统
JP6110854B2 (ja) ガス・タービン・エンジンで使用するための予混合燃料空気を用いた接線方向環状燃焼器
CN104053883B (zh) 混合用于在燃气涡轮发动机内燃烧的燃烧反应物的方法
US20160265779A1 (en) Twin radial splitter-chevron mixer with converging throat
US11708973B2 (en) Combustor
US11041623B2 (en) Gas turbine combustor with heat exchanger between rich combustion zone and secondary combustion zone
EP2587159B1 (de) Kraftstoffeinspritzanordnung zur Verwendung in Turbinenmotoren und Verfahren zu deren Zusammenbau
CN116291869A (zh) 具有稀释开口的燃烧器
CN103930721A (zh) 用于燃气涡轮机使用的切向且无火焰的环形燃烧器

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150617